N979AT

Part: NONE — NONE (NONE) · airframe 60,712 hrs · 43,806 cycles

SHIP 9544 REPETITIVE INSPECTIONS WITHIN FORTY-SIX HUNDRED (4,600) FLIGHT CYCLES UPON ER/A 617313-14. CORRECTIVE ACTION: C/W REPAIRED PER ERA 617313 (1255743).

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 60,712 hrs · 43,806 cycles

SHIP 9544 ACCOMPLISH ER/A 617313-14 REV A. CORRECTIVE ACTION: REPARIED PER ER/A 14-617313. (1255302)

Part: FUEL CELL — LEAKING (ZONE 600) · airframe 59,314 hrs · 42,511 cycles

-AD- FUEL LEAK FOUND DURING INSPECTION OF THE RH WING AFT LOWER SKIN BTW STA XRS 154 TO STA XRS 164, AFT EDGE BTW LOWER PRODUCTION DOUBLER AND LOWER WING SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO THE FURTHER FLIGHT. SUMMARY OF NRC 00061: RH WING AFT LOWER SKIN BTW STA XRS 154 TO STA XRS 164, AFT EDGE BTW LOWER PRODUCTION DOUBLER AND LOWER WING SKIN WAS REPAIRED PER ERA 622334-14AD REV ORIGINAL SECTION I PERMANENT REPAIR. TIME CONTROLLED ITEM WILL BE FOLLOWED UNDER LOG PAGES 0822756 AND 0822728. ASSOCIATED AA 5720-01103 ADDED FOR AC 9544. ASSOCIATED ER/A 14-622334 ADDED FOR AC 9544. (LP #0823065)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 59,493 hrs · 42,660 cycles

-AD- DAMAGE TOLERANCE EVALUATION, ER/A 622334-14 SECT II WITH AMOC TO AD 2024-21-01. DTA MONITOR INSPECTION REQUIRES DTA / AMOC APPROVAL BEFORE THE 1ST OF 30 DAYS OR 177 CYCLES. CONTACT MSP LIAISON ENGINEERING. DISCONTINUE REVENUE SERVICE ON OR BEFORE 30 DAYS OR 177 CYCLES PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW WITH AMOC. ASSOCIATED AA 5720-01103 ADDED FOR AC 9544. ASSOCIATED ER/A 00-622334 ADDED FOR AC 9544. **REDEFERRED LOG TO QC, ESTAB MON INSP** 10-0557-8-9588 COMPLIED WITH ER/A 622334-14AD REV A. REFER TO LOG #0872418 FOR ER/A 622334-14AD REV A REPETITIVE INSPECTIONS. CLOSED LOG AND REMOVED MONITOR INSPECTION. (LP #0822756)

Part: CABLE — OUT OF POSITION (TAIL CONE DEPLOY) · airframe 59,302 hrs · 42,501 cycles

TAILCONE DEPLOYMENT SYSTEM CABLE OUT POSITION OF PULLEY STA 1225 IN 2 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00952: CABLE ROUTED AND GUARD PIN WAS INSTALLED CORRECTLY ON PULLEY STA 1225 IN THE 2 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT PER BOEING 717-200 AMM 20-00-02 911-805. (LP #0809489)

Part: HINGE FITTING — CORRODED (ZONE 500 FLAP) · corrosion level 2 · airframe 60,662 hrs · 43,754 cycles

IN REFERENCE TO NRC 00309: AFTER REMOVAL SEALANT WAS FOUND CORROSION ON CENTER FLAP HINGE AT LH WING. CENTER WING FLAP HINGE FITTING WAS REMOVED PER B717 AMM 57-55-25-000-802 AND CENTER WING FLAP HINGE (0797513)

Part: RETAINER — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00468: CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622332-14 REV 1 AND ER/A 622332-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-622332 ADDED FOR AC 9544. (LP #0790168)

Part: DRAIN — CRACKED (WINDOW FRAME) · airframe 59,302 hrs · 42,501 cycles

CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00027: CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622331-14 REV 1 AND ER/A 622331-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-622331 ADDED FOR AC 9544. (LP #0786221)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACK ON FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 264: FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-30-08-2R PROCEDURE 7 REPAIR 7. (LP #0767385)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00839: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT WERE REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. PERFORM AN INITIAL VISUAL INSPECTION AT 25,000 FLIGHT CYCLES, THEN EVERY 6,000 CYCLES PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3, PARAGRAPH 6. A. TABLE 205. (LP #0762667)

Part: PAN — WORN (ZONE 100) · airframe 59,302 hrs · 42,501 cycles

WEAR ON INNER PAN FWD LOWER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00083: INNER AND OUTER PAN FWD EDGE LOWER CORNER OF FWD CARGO DOOR WAS REPAIRED PER PRI 622673-14 REV 4 AND ERA 622673-14, SECTION I, PERMANENT REPAIR, REV ORIGINAL. ASSOCIATED ER/A 14-622673 ADDED FOR AC 9544. (LP #0759992)

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

-AD- CORROSION ON FWD BULKHEAD OF LH WHEEL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS). SUMMARY OF NRC 00140: CORROSION LEVEL 2. CORROSION ON FWD BULKHEAD OF LH WHEELL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS) WAS REPAIRED PER PRI 622787-14 REV 3 AND ER/A 622787-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-622787 ADDED FOR AC 9544. (LP #0753504)

Part: SKIN — DAMAGED (ZONE 300) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION AND TOOL MARKS WERE FOUND ON INNER HOLE #27 AND WEAR ON UPPER SKIN AROUND FROM #27 AT RH HORIZONTAL STAB. SUMMARY OF NRC 00735: CORROSION LEVEL 2. CORROSION IN HOLE #27 AT RH HORIZONTAL STAB WAS REPAIRED PER PRI 622779-14 REV 2 & ER/A 622779-14 REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 24DEC24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIERED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIERED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93. (REFRENCE LOG PAGE 0748181). ASSOCIATED ER/A 14-622779 ADDED FOR AC 9544. (LP #0753609)

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 59,302 hrs · 42,501 cycles

SCRATCHES AND MISSING MATERIAL WERE FOUND ON INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER. SUMMARY OF NRC 00729: INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER WAS REPAIRED PER PRI 622781-14 REV 2 & ER/A 622781-14 REV ORIGINAL. ASSOCIATED ER/A 14-622781 ADDED FOR AC 9544. (LP #0753402)

Part: STRUCTURE — DAMAGED (ZONE 300) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION AND SCRATCHES ON INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB. SUMMARY OF NRC 00742: LEVEL CORROSION 2. CORROSION IN INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB WAS REPAIRED PER PRI 622843-14 REV 1 & ER/A 622843-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 17DEC24. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE ANALYSIS (DTA) STAGES II AND III ARE REQUIRED IN ACCORDANCE WITH PROCEDURES STABLISHED IN FAA AC 120-93 (REF LOG PAGE # 0717255) ASSOCIATED ER/A 14-622843 ADDED FOR AC 9544. (LP #0753545)

Part: SKIN — DAMAGED (ZONE 100) · airframe 59,302 hrs · 42,501 cycles

-AD- ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50, ALSO ON SAME ANGLE BTW X=44 AND X=50 (4 EA) AT WINGBOX AREA. (CPAX). SUMMARY OF NRC 00750: ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50 AT WINGBOX AREA WERE REPAIRED PER PRI 562343-14 REV 2 AND ER/A 562343-14AD REV A SECTION II: PERMANENT REPAIR AND ANGLE BTW X=44 AND X=50 WAS REPLACED AND INSTALLED PER DWG 3916418 REV A AND B717-200 SRM 51-41-05-0G UNDER LOG PAGE 0753504. ASSOCIATED ER/A 14-562343 ADDED FOR AC 9544. (LP #0753725)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

-AD- CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-01D). SUMMARY OF NRC 0470: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, 51-41-01-0G, AND CARD 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9544. (LP #0747957)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ALONG CARGO TRACK RH AT AFT CARGO COMPARTMENT. SUMMARY: CORROSION LEVEL 2. CORROSION ALONG TRACK RH BTW STA Y=813 TO STA Y=954, AT AFT CARGO COMPARTMENT WAS REMOVED PER B717-200 SRM 51-10-04-0G. (UT) THICKNESS MEASUREMENT WAS ACOMPLISHED WITH ORIGINAL THICKNESS OF 0.060 IN, REMAINING THICKNESS .0025 IN. THEREFORE, IT IS OUT LIMITS PER B717-200 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 AND SRM 53-00-00-1A PROCEDURE ALLOWABLE GENERAL. NEW TRACK WAS DRILLED AND ADJUSTED PER B717-200 SRM 51-40-08-0G AND WAS INSTALLED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0744855)

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ON DOOR JAMB PAN. ALSO ON PREVIOUS REPAIR DOUBLER AT AFT CARGO COMPARMENT BTW STA Y=954 TO STA Y=994 APROX C2. SUMMARY OF NRC 00133: CORROSION LEVEL 2. DOOR JAMB PAN AT AFT CARGO COMPARTMENT BTW STA Y=954 TO STA Y=994 APPROX C2 WAS REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7. (LP #0741401)

Part: SKIN — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACK ON AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT. SUMMARY OF NRC 00707: AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 AND FIXED UPPER FLIGHT COMPARTMENT WINDOW RH WAS INSTALLED UNDER NRC 00667. (LP #0735202)

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ON TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA). SUMMARY OF NRC 00722: CORROSION LEVEL 2. TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #0725967)

Part: PIN — OUT OF POSITION (ZONE 800) · airframe 59,302 hrs · 42,501 cycles

THE INFLATION CABLE PIN WAS OUT OF PLACE. ALSO MISSING THE VALVE LOCK PIN ON THE FWD PASSENGER ENTRANCE DOOR SLIDE (L1). THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00065: SLIDE ASSEMBLY OF L1 DOOR WITH WAS REPLACED BY A SERVICEABLE SLIDE ASSEMBLY UNDER AMDS 2561-9004 AND AMDS 97-2561-9-0003 ON LP #0717411. (LP #0725539)

Part: CUSP WEB — CRACKED (ZOEN 200) · airframe 59,302 hrs · 42,501 cycles

CRACK ON CUSP WEB BTW STA Y=636-655 X=- 44 TO X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 826: CUSP WEB BTW STA Y=636-655 X=-44 TO X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0721136)

Part: STOP FITTING — CRACKED (ZONE 800) · airframe 59,302 hrs · 42,501 cycles

DOOR STOP FITTING #4 WAS FOUND CRACK ON INNER PAN FWD SIDE OF AFT CARGO DOOR. SUMMARY OF NRC 00716: INNER PAN ON FWD SIDE STOP #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 622684-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622684-14 REV 1. ASSOCIATED ER/A 14-622684 ADDED FOR AC 9544. (LP #0717281)

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927. SUMMARY OF NRC 00725: CORROSION LEVEL 2. CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR 6 FIG 208. (LP #0713769)

Part: FRAME — CRACKED (ZONE 100) · airframe 59,302 hrs · 42,501 cycles

CRACK ON FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00579: FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-0G PROCEDURE 4 REPAIR 4. (LP #0709303)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACKED LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX). SUMMARY OF NRC 00580: LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0706823)

Part: BEAM — CRACKED (ZONE 800) · airframe 59,302 hrs · 42,501 cycles

CRACK ON INTERNAL STRUCTURE LL BEAM #1 STA 195 AT PASSENGER DOOR. SUMMARY OF NRC 00293: BEAM #1 ON INTERNAL STRUCTURE STA 195 AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0703468)

Part: FRAME ANGLE — CRACKED (ZONE 400) · airframe 59,302 hrs · 42,501 cycles

CRACK ON FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH. SUMMARY OF NRC 00536: FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH WAS REPAIRED PER ERA 622468-14 REV ORIGINAL. (LP #0703045)

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACK ON CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00606: CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 221. (LP #0703712)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACKED LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX) SUMMARY OF NRC 00581: LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2. (LP #0703457)

Part: CUSP WEB — DAMAGED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

TOOL MARK ON CUSP WEB AND SPLICE BTW STA Y=794, X44 TO X54 AT CABIN PASENGER. SUMMARY OF NRC 00547: CUSP WEB ON STA 796 X44 TO X54 WAS REPAIRED PER B717 SRM 53-00-55-2R. (LP #0700055)

Part: LONGERON — CRACKED (ZONE 200) · airframe 59,302 hrs · 42,501 cycles

CRACK ON LONGERON 17 LH, LONGERON 8 LH, AND LONGERON 13 LH BTW STA Y=1020 AND STA Y=1023 LH SIDE. SUMMARY OF NRC 537: LONGERON 17 LH AND LONGERON 8 LH BTW STA Y=1020 AND STA Y=1023 LH WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2. AND LONGERON 13 LH HAD NO CRACKS FOUND PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001. PERFORM AN EXTERNAL GVI EVERY C-CHECK PER B7171 SRM 53-00-05-2R- 2 STEP (7) TABLE 202. **REDEFFERED LOG TO QC, ESTABLISHED MONITOR INSP **. (LP #0695566)

Part: DOUBLER — CRACKED (ZONE 100) · airframe 59,302 hrs · 42,501 cycles

CRACK ON EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1). SUMMARY OF NRC 00088: EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1) WAS FABRICATED AND REPLACED PER B717-200 SRM 52-30-01-2R PROCEDURE 1 REPAIR 1 PAR. 4B (9), (10), AND (11). (LP #0696773)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ON SEAT TRACK X=56 AND STA 996 IN PAX CABIN. SUMMARY OF NRC 723: CORROSION LEVEL 2. SEAT TRACK X=56 AND STA 996 IN PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1 FIGURE 201. PERFORM DECAL INSPECTION CONDITION EVERY C-CHECK PER TOPP 30-10-70 PAGE 14 PAR I. DEFERRED TO DECAL CONDITION MONITOR PER TOPP 30-10-70 TO BE INSPECTED AT THE APPROPRIATE CHECK INTERVAL. (LP #0694490)

Part: DOUBLER — CORRODED (STA 1053) · corrosion level 2 · airframe 59,302 hrs · 42,501 cycles

CORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00563: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD WAS REPLACED PER B717 SRM 53-20-08-0I PROCEDURE 2 AND 51-41-05-0G. (LP #0684614)

Part: VANE — DENTED (ZONE 600 FLAP) · airframe 59,302 hrs · 42,501 cycles

-AD- DENTS ON RH WING FWD MOVABLE VANE INBD SURFACE. SUMMARY OF NRC 00326: DENTS (3 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE RH WING WERE EVALUATED AND FOUND OUT LIMITS. RH WING FWD MOVABLE VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR. 4. D. (LP #0661904)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 58,044 hrs · 41,396 cycles

-AD- VERTICAL STAB LEFT SIDE 4 EA HOLES HAVE CRACK INDICATIONS, IN SKIN LAYER ONLY, JUST BELOW ZFS 52.267. BHEC INSP CONFIRMS CRACKS IN 4 EA HOLES IN SKIN LAYER ONLY REF AA 5530-01048 AND AD 2018-10-08 -MARKED-. COMPLIED WITH PRI 617313-14AD REV 0. C/W PRI 617313-14AD REV 1. C/W PRI 617313-14AD REV 2. C/W ER/A 617313-14AD REV ORIG SEATION I PERMANENT REPAIR. ENSURED ER/A 6171313-14AD REV ORIG MATCHES PRI 617313-14AD REV 0, 1, AND 2. ASSOCIATED ER/A 14-617313 ADDED FOR AC 9544. (LP #0297160)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 58,044 hrs · 41,396 cycles

-AD- FOUND 4 EA HOLES ON LT VERT BELOW EXISTING DOUBLER AT SPLICE SHOWING CRACK INDICATIONS. C/W ER/A 617313-14AD REV ORIG SECTION I PERMANENT REPAIR. ALL RII C/W (QC1430) REF TO LOG PAGE 0297160 AND BUFF NRC 001. ASSOCIATED ER/A 14-6173133

Part: LENS — MISSING (SEAT 2B) · airframe 57,514 hrs · 40,965 cycles

CABIN EMERGENCY LIGHT LENS MISSING AT 2B. MAINTENANCE FOUND STAND-BY OVERHEAD EMERGENCY LIGHT COVER MISSING AT ROW 2. INSTALLED THE LIGHT COVER AS REQUIRED REF B717 AMM 33-51. AIRCRAFT IS OK FOR SERVICE. (LP #0160810)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,951 hrs · 40,490 cycles

ELONGATED AND CRACKED HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L IN REF NRC 00086. SUMMARY OF NRC 00123: DAMAGE IN HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L WAS REPAIRED PER B717-200 SRM 53-03- 01-2R REPAIR I. PAR. 6 J. FIG. 211. (LP #0026494)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,945 hrs · 40,486 cycles

SEVERAL DENTS ON UPPER SKIN ON AFT MOVABLE FLAP VANE AT LH WING. SUMMARY OF NRC 00053: UPPER SKIN ON AFT MOVABLE FLAP VANE AT LH WING WAS REPAIRED PER ER/A 612869-14 REV ORIGINAL. ASSOCIATED ER/A 14-612869 ADDED FOR AC 9544. (LP #0025737)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,945 hrs · 40,486 cycles

CRACK ON PAN AT AFT CARGO DOOR 994 BTW BEAM 1 TO 2. SUMMARY OF NRC-0087: INNER AND OUTBOARD PAN AT AFT CARGO DOOR 994 BTW BEAM 1 TO 2 WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8, REPAIR 8, PAR 4. (LP #0024588)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,865 hrs · 40,412 cycles

FOUND INTERCOSTAL CRACKED BETWEEN STA 946.5 AND 954. FABBED NEW INTERCOSTAL PER DWG 9915578 AND SRM 53-20-51-0I PROC 7. INSTALLED INTERCOSTAL PER B717 SRM 51-41. (LP #2980699)

Part: PANEL — DAMAGED (CABIN FLOOR) · airframe 55,420 hrs · 39,205 cycles

PANEL DAMAGED AND BENT. REPAIRED AND FABRICATED PANEL.

Part: BATTERY — INOPERATIVE · airframe 54,127 hrs · 38,001 cycles

THE OVER WING EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. MAINTENANCE REPLACED THE FWD OVER WING EMERGENCY EXIT LIGHT BATTERY ASSEMBLY PER B717 AMM 33- 11. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #8967630)

Part: NONE — NONE · airframe 53,977 hrs · 37,861 cycles

SHIP 9544 - THE FLIGHT CREW RETURNED THE AIRCRAFT BACK TO ATL DUE TO MULTIPLE "FIRE DETECTION FAIL" MESSAGES. AN EMERGENCY WAS DECLARED WITH ATC. NO SECONDARY INDICATION OF A FIRE ON ANY ENGINE GAUGE. CORRECTIVE ACTION: MAINTENANCE FOUND A LOOSE CONNECTOR AT THE FIREWALL. THE CONNECTOR WAS SECURED AND AN OPERATIONAL CHECK WAS GOOD. BOTH VIA AND THE FIRE DETECTION SYSTEM CONTROL UNIT WERE REPLACED AS A PRECAUTION. A SUCCESSFUL VERIFICATION FLIGHT WAS PERFORMED. (LP #9275812)

Part: CONTROL UNIT — INOPERATIVE (NR 2 FIRE DETECT) · airframe 52,837 hrs · 36,837 cycles

SHIP 9544 -DIV- TO RDU WITH A RIGHT ENGINE SPURIOUS FIRE INDICATION. CORRECTIVE ACTION: REPLACED #2 VIA, FDCU AND PERFORMED ENGINE DUCT LEAK CHECKS AND ALL RETURN TO SERVICE CHECKS.

Part: NONE — NONE · airframe 52,593 hrs · 36,628 cycles

THE CABLE END OF THE TAILCONE EXIT HANDLE AT 900 POS IS BENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/002 00392: MAINTENANCE REPLACED CABLE FOR TAILCONE EXIT HANDLE REF B717 AMM 53-52-01. (LP #2016031)

Part: NONE — NONE · corrosion level 2 · airframe 52,572 hrs · 36,609 cycles

R1 DOOR GIRT BAR FLOOR STRUCTURE CORRODED. -MKD- SUMMARY SEE NRC 001-0375:5211-2001/006 00171: CORROSION LEVEL 2, REPLACED FITTINGS REF B717 SRM 51-40-02 AND BOEING DWG 3936190. (LP #2005863)

Part: FORMER — CRACKED (ZONE 100) · airframe 58,571 hrs · 41,868 cycles

CRACKED LH AND RH FORMERS AT STA Y=715 AT KEEL BEAM AREA. (FUS) SUMMARY OF NRC 00341: FORMERS WERE REPAIRED PER B717 SRM 51-70-11-2R-1 FIG 201. (ET) HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREAS AT RH & LH FORMERS, NO CRACKS WERE FOUND PER DC-MD/BOEING NDTSPM PART 6, 06-10-01.001 (EQUIPMENT: NORTEC 600D C.N.1601 DUE DATE: 01/MAR/18). (LP #0272628)

Part: LIGHT — UNSECURE (CABIN) · airframe 47,826 hrs · 32,652 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE LOCATIONS:19B. SECURED LIGHTING STRIP. OK FOR SVC. REF AMM 33-51. (LP1162517)

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 47,826 hrs · 32,652 cycles

AFTER SELECTING APU BLEED AIR ON WITH BOTH LEFT OR RIGHT PACK ON, FUEL ODOR IN AIRCRAFT , DISSIPATED AFTER A FEW MINUTES. STARTED ODI PREVENTION -AMM 2172. INSPECTED APU - RAN PAKS FOUND NO CONTAMINATION AT APU COMPARTMENT OR THE INLET. PER FIM 49-50-00-810-807 FOUND BOTH PACK SYSTEM COALESCER BAGS AND CLEANED HOUSING . X 2 AND PAK BURN OUT PER AMM 21-54. COMPLETED ALL NO GO ODI PREVENTION PROGRAM PER ATA 2172. M/C NOTIFIED OK FOR SERVICE. (LP5948933)

Part: LIGHT — DAMAGED (CABIN) · airframe 47,693 hrs · 32,541 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT 19B. 19B EMERGENCY LIGHT DAMAGED OR INOPERATIVE LIGHT ASSY - PHOTO LUMINESCENT [LENGTH 23.90 INCHES] REF IPC 33-51-12-01 ITEM 55. MAINTENANCE REINSTALLED PHOTO LUMINESCENT STRIP REF LOG PAGE #5917548. (LP #1120925)

Part: DOOR — DAMAGED (NLG) · airframe 47,070 hrs · 32,067 cycles

LEFT NOSEGEAR DOOR FOUND DAMAGED ON ARRIVAL. ACCOMPLISHED DVI PER NTM51-90-00 OF THE LOCAL AREA. NO OTHER DAMAGE NOTED. REMOVED DAMAGED DOOR PER ERA576579-14 REV O. INSTALLED -509 S/N DL18 AFT LEFT NLG DOOR PER AMM32-20-01 AND ERA576579-14 REV O. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 10 DAYS. OK FOR SERVICE. DEFERRED DUE TO SHORT GROUND TIME AND REQUIREMENT TO JACK AND RETRACT/EXTEND LANDING GEAR FOR DOOR ADJUSTMENT. (LP5840244)

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 46,645 hrs · 31,799 cycles

THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN. MAINTENANCE REPLACED THE KEVLAR CABLE PER IPC 53-52-30-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-2001 TAILCONE SERVICE. FUNCTIONAL CHECK WAS SATISFACTORY. (LP #0918007)

Part: SCUFF PLATE — DAMAGED (FUSELAGE) · airframe 46,660 hrs · 31,809 cycles

DAMAGE TO AFT CARGO SCUFF PLATE IS OUT OF SRM LIMITS AND MUST BE REPLACED. REMOVED DAMAGED THRESHOLD AND INSTALLED NEW THRESHOLD AND SEALED PER SRM 51-41-01. (LP #5546720)

Part: COVER — LOOSE (EVAC SLIDE) · airframe 46,571 hrs · 31,746 cycles

TAILCONE SLIDE COVER IS LOOSE. MAINTENANCE REMOVED THE TAILCONE SLIDE PER W/C 5261-9006. FOUND SLIDE COVER ASSEMBLY RECEIVER HITCH TO BE WORN. COVER PITT PIN WILL NOT STAY LATCHED. THE TRAY ASSEMBLY WAS REPLACED AND THE NEW SLIDE WAS INSTALLED PER AMDS 2561-9006. (LP #3791294)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,570 hrs · 30,349 cycles

FOUND SKIN DAMAGE AT APPROX STATION 200 AND LONGERON 17R. DENT IS 0.210" DEEP, 12 INCH LONG, WITH A MAX DIAMETER OF 1.5". FOUND TO BE OUT OF LIMITS PER SRM 53-01-01-1A3. REPAIR ACCOMPLISHED ON NRC 004, LOG 0504045.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,570 hrs · 30,349 cycles

SKIN DAMAGE AT APPROX STATION 200 LONGERON 17R. DENT FOUND TO BE .210 DEEP 12" LONG MAX DIA. 1.5" - OUT OF LIMITS PER SRM 53-01-01-1A3. REMOVED DAMAGE PER SRM 53-03-01-2R-1 FIG 205. FABRICATED, DRILLED, AND INSTALLED DOUBLER PER SRM 53-03-01-2R-1 FIG 205.

Part: DOUBLER — CORRODED (BS 968-978) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON INTERNAL DOUBLER BETWEEN BS 968 TO 978 AT THE LWR CARGO DOOR FRAME. THE DOUBLER WAS REPAIRED IAW ETI 17-17-205, REV 3, AND ER/A 562358-14, REV ORIG.

Part: LONGERON — CORRODED (BS 900-1006) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON CARGO BAY LONGERON 30, BS 900 - 1006. THE LONGERON WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05.

Part: FRAME ANGLE — CORRODED (BS 908) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON FRAME ANGLE, BS 908 BETWEEN LONGERONS 26R TO 26L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-20-07-01-3, 51-41-02 0G, AND 51-41-05 0G.

Part: DOOR FRAME — CORRODED (BS 954-994) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON THE AFT LOWER CARGO DOOR FRAME BETWEEN BS 954 AND 994. THE DOOR FRAME WAS REPAIRED IAW ER/A 562361-14, REV ORIG, AND ETI-17-17-203, REV 3.

Part: RUB STRIP — CORRODED · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION AND DISBONDED RUB STRIPS AT THE LT AND RT SIDE ON FILLET PANELS. THE RUBSTRIPS WERE REPLACED IAW SRM 53-20-70-01, AND 51-20-05-0G.

Part: SEAT TRACK — CORRODED (BS 110-140) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON COCKPIT RT SEAT TRACK BETWEEN BS 110 AND 140, RBL 44. DAMAGED AREA WAS REPAIRED IAW ER/A 562373-14, REV ORIG, AND ETI-17-17-215, REV 1.

Part: DRAG BRACE — CORRODED (NLG) · airframe 43,491 hrs · 29,530 cycles

CORROSION ON TAPER PIN AND DRAG BRACE AT NOSE LANDING GEAR IN REF CARD 3230-5002 STEP 13. LEVEL CORROSION 2. NOSE LANDING GEAR DRAG BRACE LINK ASSY WAS REPLACED PER AMM 32-22-05 AND TESTS OK.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

EXCESSIVE CORROSION ON FRAME BTW LONG 27R AND 27L STA Y=974 AT AFT CARGO COMPARTMENT. LEVEL CORROSION 2. DAMAGE AREA WAS REPAIRED PER SRM 53-20-07-2R-3 FIG 201 (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FRAME BTW LONG 27R AND 27L STA Y=974 AT AFT CARGO COMPARTMENT. NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 43,491 hrs · 29,530 cycles

CRACK INDICATIONS IN RT SIDE VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE OPEN HOLES AT STA ZFS=52.700, ZFS=51.767, ZFS=50.767, ZFS=49.767, ZFS=48.767 (5530-01048-01) (AD 2016-0905)(SM). RT SIDE VERTICAL STABILIZER FRONT SPAR CAP WAS REPAIRED PER ER/A 541681-14AD REV C SECTION III. ETI -17-17-196 REV 3.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON FRAME CLIP IS OUT OF LIMITS, STA Y=927 BTW LONG 25L TO 25R AND STA Y=974, STA Y=994 BTW LONG 25L TO 29R AT AFT CARGO COMPARTMENT IN REF NRC 307 (C2). LEVEL CORROSION 2. FRAMES CLIPS WERE REPLACE PER SRM53-20-07-0I-3, 51-41-02-0G, AND 51-41-05-0G.

Part: STRUCTURE — CORRODED (BS 737-756) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION OUT OF LIMITS ON UPPER SURFACE OF CENTER TANK AT LT SIDE, BETWEEN BS 737 TO 756, LBL 54 TO 60. REPAIRED IAW ERA 562343-14.

Part: WEB — CORRODED (BS 200) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON WEB, BS 200, LONGERON 18L LBL 56, Z=2. REPAIRED IAW SRM 51-70-10-2R-2.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 43,491 hrs · 29,530 cycles

FLOOR PANEL 221NF FOUND DAMAGED BEYOND LIMITS. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2, FIG 201.

Part: CUSP WEB — CRACKED (BS 889-908) · airframe 43,491 hrs · 29,530 cycles

CRACK ON THE LEFT CUSP WEB BS 889 - 908, BETWEEN LBL 54 TO 60. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND 53-00-55-2R-4, FIG 226.

Part: LONGERON — CRACKED (BS 1133) · airframe 43,491 hrs · 29,530 cycles

CRACK ON LONGERON 2L, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, FIG 201, SHEET 2.

Part: VANE — WORN (RT WING TE FLAP) · airframe 43,491 hrs · 29,530 cycles

WEAR ON THE RT WING FLAP VANE INBD EDGE XRS 137. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01-2R-1, REP 1.

Part: WEB — PUNCTURED (BS 201) · airframe 43,491 hrs · 29,530 cycles

PUNCTURE WAS FOUND ON THE WEB AT BS 210, RBL 2. REPAIRED IAW SRM 51-70-10-2R.

Part: CUSP WEB — CORRODED (BS 400-465) · airframe 43,491 hrs · 29,530 cycles

CORROSION OUT OF LIMITS ON THE RT CUSP WEB BETWEEN RBL 44.5 TO 60, BS 400- 402, 408- 427, AND 446 - 465. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4, FIG 216, & SRM 51-41-02.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION WAS FOUND ON BARREL NUT HOLE UPPER SURFACE NR 28 AT RT HORIZONTAL STABILIZER CENTER BOX SKIN. BARREL NUT HOLE NR 28 WAS REPAIRED IAW ETI-17-17-195 REV. 1 AND ERA 562347-14.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 43,491 hrs · 29,530 cycles

A CRACK WAS FOUND ON THE ANGLE FWD EDGE BEAM NR 3 INTERNAL STRUCTURE AT THE AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-05.

Part: CUSP WEB — CORRODED (BS 834-835) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION OUT OF LIMITS ON THE RT CUSP WEB BETWEEN RBL 44.5 TO RBL 60, BS 834 TO 835. THE CUSP WEB WAS REPAIRED.

Part: SKIN — DELAMINATED (RUDDER TAB) · airframe 43,491 hrs · 29,530 cycles

SKIN ON RUDDER CONTROL TAB TRIM TAB WAS FOUND DELAMINATED, IAW SRM 51-70-02-0G PARAG 8 A (2) AND NDT SPM 04-00-00 PARAG 2 D (1). THE SKIN ON RUDDER CONTROL TAB TRIM TAB WAS BONDED IAW SRM 51-70-02-2R-7, PAR.4 B, STEP 14 AND 16.

Part: PAN — WORN (BULKHEAD DOOR) · airframe 43,491 hrs · 29,530 cycles

WEAR ON PAN AND LT ANGLE AT THE AFT CABIN BULKHEAD DOOR. THE PAN WAS REPAIRED AND ANGLE WAS REPLACED IAW SRM 52-10-02-2R-15, AND DWG 9929480, REV BW.

Part: STOP FITTING — CORRODED (BULKHEAD DOOR) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON THE LT LOWER STOP AT THE AFT CABIN BULKHEAD DOOR. THE STOP WAS REPLACED IAW SRM 51-41-01.

Part: CUSP WEB — CRACKED (BS 715-720) · airframe 43,491 hrs · 29,530 cycles

CUSP WEB, BS 715 - 720, RBL 44 - 50 CRACKED. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.

Part: FORMER — CRACKED (BS 680) · airframe 43,491 hrs · 29,530 cycles

CRACKED FORMER AT BS 680 AT KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1, FIG 201.

Part: SEAT TRACK — CORRODED (BS 200-257) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON THE RT SEAT TRACK RBL 22, BS 200 TO 257. THE SEAT TRACK WAS REPLACED IAW SRM 53-20-52-2R-5.

Part: FORMER — CRACKED (BS 694) · airframe 43,491 hrs · 29,530 cycles

CRACKED FORMER AT BS 694 . THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1, FIG 201. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREAS, NO CRACKS WERE FOUND IAW NDTSPM PART 6, 06-10-01.001.

Part: SEAT TRACK — CORRODED (BS 200-246) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

SEAT TRACK RBL 44, BS 200 - 246 CORRODED. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-20-52-2R-5.

Part: SHEAR TIE — CRACKED (BS 1022) · airframe 43,491 hrs · 29,530 cycles

CRACKED SHEAR TIE BS 1022 BETWEEN STRINGERS 4 - 5L. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.

Part: FRAME — CRACKED (BS 1037) · airframe 43,491 hrs · 29,530 cycles

CRACK ON FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R-4. PERFORMED A HFEC INSPECTION, NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDTSPM 06-10-01.001.

Part: FRAME — CRACKED (BS 946) · airframe 43,491 hrs · 29,530 cycles

CRACKED RH RING PAN AFT/LOWER CORNER BS 946, FASTENERS AND AREA DAMAGE WERE REMOVED IAW SRM 51-41-02, 51-41-05, AND 56-20-02-2R. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW NDT SPM 06-10-01.001. . REPAIR FABRICATED IAW SRM 56-20-02-2R. AND INSTALLED IAW SRM 51-41-02 AND 51-41-05.

Part: FRAME — CRACKED (BS 908) · airframe 43,491 hrs · 29,530 cycles

CRACKED RT RING PAN AFT/UPPER CORNERS BS 908. : FASTENERS AND AREA DAMAGE REMOVED IAW SRM 51-41-02, 51-41-05, AND 56-20-02-2R. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. A REPAIR WAS FABRICATED IAW SRM 56-20-02-2R, AND INSTALLED IAW SRM 51-41-02 AND 51-41-05.

Part: BEAM — CRACKED (NR 6) · airframe 43,491 hrs · 29,530 cycles

CRACKED NR 6 BEAM MID POSITION JUST AROUND BOLT AT THE FWD PASSENGER DOOR. THE DAMAGE WAS REPAIRED IAW ER/A 559578-14MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 389) · airframe 43,491 hrs · 29,530 cycles

CRACKED OUTER PAN ON BS 389 AND NR 5 BEAM AT FWD CARGO BAY DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-1, FIG 201.

Part: RETAINER — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 43,491 hrs · 29,530 cycles

CORROSION ON LOWER SEAL RETAINER AT FWD R1 SERVICE DOOR. THE SEAL RETAINER WAS REPLACED SRM 51-41-01-0G.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 43,398 hrs · 29,464 cycles

EMERGENCY EXIT DIFFUSER LENS UNSECURE. SECURED THE LENS IAW AMM 33-51. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 43,371 hrs · 29,450 cycles

EMERGENCY EXIT SIGN COVER LOOSE. INSTALLED EXIT SIGN. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,806 hrs · 25,972 cycles

EMERGENCY LIGHTS AT L1 DOOR OVERHEAD AND EXIT SIGN BY FLIGHT DECK DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 38,806 hrs · 25,972 cycles

DURING CHECK VISIT, FOUND VERTICAL STABILIZER L/E LOWER 2 ROWS OF FASTENERS AT ZFS 66.6 PULLED THRU SKIN, APPROXIMATELY 12" IN LENGTH ON LT SIDE. REPAIRED IAW ER/A 541681-14.

Part: SKIN — WORN (VERTICAL STAB) · airframe 38,806 hrs · 25,972 cycles

DURING C-CHECK, FOUND VERTICAL STABILIZER LOWER FIXED L/E SKIN INTERNAL FINGER DOUBLER WORN. REPAIRED IAW DWG SG-95550001, SRM 55-30-01, AND ER/A 541681-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,801 hrs · 25,965 cycles

ER/A 532116-14, REV A SECTION II WAS ACCOMPLISHED DURING C-CK IN MSP TO ADDRESS GROUND DAMAGE TO FUSELAGE SKIN JUST BELOW AND AFT OF L1 DOOR, PREVIOUSLY REPAIRED IAW SECTION I.

Part: PAN — CORRODED · corrosion level 2 · airframe 38,801 hrs · 25,965 cycles

AFT CARGO LOWER PAN HAS CORROSION ON FWD SPLICE DOUBLER, LOWER LEG. R & R LOWER SPLICE ANGLE. ALL WORK PERFORMED AND COMPLETED SRM 53-20-15, REPAIR 7.

Part: SUPPORT — CRACKED (SLAT DRIVE) · airframe 38,801 hrs · 25,965 cycles

RT SLAT DRIVE, AFT SUPPORT CRACKED AT BEARING ASSY LOWER FASTNER HOLES. REMOVED RT SLAT DRIVE ASSY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,588 hrs · 25,813 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,835 hrs · 25,171 cycles

DURING LINE CHECK, FOUND AFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND OPS NORMAL.

Part: SKIN — DAMAGED (BS 215) · airframe 36,825 hrs · 24,342 cycles

DAMAGE DISCOVERED APPROXIMATELY 18 INCHES AFT OF L1 DOOR, APPROXIMATELY 2 FT BELOW FLOOR LONGERON. DAMAGE IS APPROX 2.5 INCHES LONG, .5 INCHES WIDE AND APPROX .0937 INCHES DEEP. REPAIRED IAW ER/A 532116-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,546 hrs · 24,099 cycles

DURING LINE CHECK, NOTED OVERHEAD COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AT BS 123. CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,365 hrs · 23,085 cycles

A PILOT REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN & CATWALK AREA WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BATTERY PACK AND OPS CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,277 hrs · 23,008 cycles

DURING LINE CHECK, FOUND FIVE EMERGENCY LIGHTS INOPERATIVE IN TAIL COMPARTMENT ALONG CATWALK. REPLACED EMERGENCY BATTERY PACK B5-260 IAW AMM 33-51. EMERGENCY LIGHTS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,176 hrs · 22,920 cycles

DURING LINE CHECK, FOUND EMERGENCY LIGHTS ON CATWALK INOPERATIVE. REPLACED POWER SUPPLY FOR EMERGENCY LIGHTS ON AFT CATWALK. OPERATION CHECKED GOOD IAW AMM 33-52.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,945 hrs · 22,718 cycles

DURING LINE CHECK, NOTED THAT EMERGENCY LIGHTS IN AFT ACCESSORY CATWALK WERE INOPERATIVE. REPLACED BATTERY PACK AT BS 1050L AND OPERATION CHECKED GOOD.

Part: DOOR FRAME — DAMAGED (BS 944-954) · airframe 43,515 hrs · 29,545 cycles

PERFORM A VISUAL INSPECTION OF THE AFT CARGO DOOR FRAME BS 944 - 954, LONGERON 27R. LOWER PAN SPLICE REPAIRED IAW SRM 53-20-15, REPAIR 7.

Part: SIGN — CRACKED (CABIN) · airframe 34,330 hrs · 22,185 cycles

OVERHEAD CEILING EMERGENCY LIGHT CRACKED AT ROW 1. R & R SIGN IAW MM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

CLIP CORRODED AT BS 1002 LONGERON 25R. R &R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SHEAR TIE CORRODED AT BS 946 LONGERON 25R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT CARGO SHEAR TIE CORRODED AT BS 946 LONGERON 27R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SHEAR TIE CORRODED AT BS 946 LONGERON 24R. R & R SHEAR TIE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT ACCESSORY COMPARTMENT LONGERON TO FRAME SUPPORT ANGLE CRACKED AT FS 1144, LONGERON 2R. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

PANEL 160GR CAMLOCK STRIP ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

CABIN AREA CUSP WEB CRACKED AT STATION 584, RBL 45. R&R WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED AT BS 636, RBL 44. R&R SEAT TRACK IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

FLOOR BOARD BRACKET CRACKED AT FS 665 RBL 22. R & R BRACKET IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

LT WING TO BODY SUPPORT CLIP CRACKED AT FS 747, LBL 7. R&R FITTING IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SHEAR TIE CORRODED AT BS 1002 LONGERON 24R. R & R SHEAR TIE IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

LONGERON CORRODED AT BS 927 LONGERON 30. REPAIRED LONGERON IAW SRM.

Part: PAN — CORRODED (CARGO BAY) · airframe 33,802 hrs · 21,849 cycles

FWD CARGO PAN CORRODED. R&R PAN IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

VERTICAL SUPPORT CRACKED AT STATION 737, RBL 44. R&R SUPPORT IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

VERTICAL SUPPORT CRACKED AT STATION 737, LBL 44. R&R SUPPORT IAW SRM.

Part: FORMER — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

LT TENSION BRACKET CRACKED AT STATION 1022. R & R FORMER IAW SRM & DRAWING.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT FUSELAGE BODY SPLICE STRAP CORRODED AT BS 813, LONGERON 29L. REPAIRED STRAP IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN STATION 900 TO STATION 1002 RBL 22. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN STATION 590 TO STATION 639, LBL 44. R&R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN BS 816 TO BS 883, RBL 44. R & R SEAT TRACK IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT CARGO FWD BULKHEAD UPPER LINER STRAP CRACKED AT BS 817 BETWEEN RBL 10 TO RBL 24. R & R STRAP IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN BS 892 TO BS 1026, LBL. R & R SEAT TRACK IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT FS BODY FAIRING ATTACH FRAME CORRODED AT BS 851 BETWEEN LONGERON 26L TO LONGERON 27L. R & R STRAP IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

RT CUSP WEB CRACKED AT BS 674. R & R WEB IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT CARGO FWD BULKHEAD BS 817 CENTER VERTICAL SUPPORT CRACKED ON LOWER END. R & R SUPPORT IAW SRM & DRAWING.

Part: DOOR — CRACKED (NLG) · airframe 33,802 hrs · 21,849 cycles

RT AFT NLG DOOR CRACKED AT AFT HINGE CUTOUT. REPAIRED DOUBLER IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN BS 813 TO BS 890, RBL 22. R & R SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

AFT CARGO FWD BULKHEAD LOWER LINER SUPPORT STRAP CRACKED AT BS 817 RBL 10. R & R INTERCOSTAL IAW SRM.

Part: DOOR — CRACKED (NLG) · airframe 33,802 hrs · 21,849 cycles

LT AFT NLG DOOR CRACKED AT AFT HINGE CUTOUT. REPAIRED DOUBLER IAW ES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN BS 256 TO BS 583, LBL 44. R & R SEAT TRACK IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 RF DELAMINATED. R & R PANEL IAW SRM.

Part: BRACKET — CRACKED (RT PYLON) · airframe 33,802 hrs · 21,849 cycles

RT PYLON LOWER TENSION BRACKET CRACKED AT BS 1022 BETWEEN LONGERON 16L TO LONGERON 17L. R & R FORMER IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

FRAME CRACKED AT FS 715 RT, BETWEEN LONGERON 18R & LONGERON 17R. R & R FRAME IAW SRM & DRAWING.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 AMF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222BF DELAMINATED. R & R PANEL IAW AMM & SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222JF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 AHF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 FF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 221UF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222ACF DELAMINATED. R & R PANEL IAW SRM.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

CUSP WEB CRACKED AT BS 674, BETWEEN RBL 54 & RBL 44. REPAIRED WEB IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 221 WF DELAMINATED. R & R PANEL IAW SRM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 33,802 hrs · 21,849 cycles

L1 DOOR INTERNAL CLIP CRACKED AFT OF DOOR HANDLE. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOOR BOARD 222 AVF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 ATF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 AEF DELAMINATED. R & R PANEL IAW SRM.

Part: SLIDE — LOW PRESSURE (TAILCONE) · airframe 33,802 hrs · 21,849 cycles

TAIL CONE ESCAPE SLIDE PRESSURE GAUGE LOW. R & R SLIDE ASSEMBLY IAW TASK CARD.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 LF DELAMINATED. R & R PANEL IAW SRM.

Part: SLIDE — CRACKED (TAILCONE) · airframe 33,802 hrs · 21,849 cycles

TAIL CONE EMERGENCY EVAC SLIDE COVER CROWN CRACKED. R & R SLIDE IAW TASK CARD.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOOR BOARD 222 APF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222PF DELAMINATED. R & R PANEL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

FRAME FITTING CRACKED AT STATION 946, STRINGER 18R. R & R FITTING IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

CUSP WEB CORRODED BETWEEN BS 598 TO BS 617 STRINGER 18R. R & R WEB IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN BS 237 TO BS 588, RBL 22. R & R SEAT TRACK IAW SRM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

CUSP WEB CORRODED BETWEEN BS 465 TO BS 484 STRINGER 18R. R & R WEB IAW SRM.

Part: BEAM — CRACKED (L1 DOOR) · airframe 33,802 hrs · 21,849 cycles

L1 DOOR INTERNAL, 7 BEAM CRACKED AT THE AFT END. R & R DOUBLER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

FRAME CRACKED AT BS 715, BETWEEN LONGERON 18L TO LONG 17L. R &R FRAME SECTION IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222AAF DELAMINATED. R & R PANEL IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 33,802 hrs · 21,849 cycles

CABIN FLOORBOARD 222 AGF DELAMINATED. R & R PANEL IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

SEAT TRACK CORRODED BETWEEN STATION 237 TO STATION 588 RBL 44. R & R SEAT TRACK IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,802 hrs · 21,849 cycles

LONGERON CRACKED AT BS 1144 LONGERON 2R. R & R LONGERON IAW SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,115 hrs · 21,426 cycles

FORWARD F/A STA LOWER FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 30,928 hrs · 20,009 cycles

R1 DOOR SLIDE DEPLOYED UNINTENTIONALLY BY CATERING OPERATOR. REMOVED AND REPLACED SLIDE PER MM.

Part: ANGLE — CORRODED (FUSELAGE)

LOWER L1 DOOR SILL ANGLE, CORROSION. ACCOMPLISHED DOOR SILL ANGLE REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-02.

Part: FASTENER — BROKEN (FUSELAGE)

FUSELAGE SKIN CLIP FASTENER, STA 1152, LONG S2R, BROKEN. ACCOMPLISHED CLIP FASTENER PLUGGED PER EA 17-53-03527IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 197, LBL 27, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-40-08 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 55, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01 AND 51-32-01.

Part: FITTING — CORRODED (GIRT BAR)

MAIN CABIN FLOOR FORWARD AND AFT SLIDE GIRT BAR LATCH FITTINGS, CORROSION. ACCOMPLISHED SLIDE GIRT BAR LATCH FITTINGS REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 202, LBL 26, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01.

Part: FASTENER — BROKEN (FUSELAGE)

FUSELAGE SKIN CLIP FASTENER, STA 1152, LONG S2L, BROKEN. ACCOMPLISHED CLIP FASTENER PLUGGED PER EA 17-53-03527IR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 148, RBL 33, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-02 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 237, BL 0, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-05, 53-20-51 AND 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-41-01 AND 53-00-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 14, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 187 TO 200, LBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 51-10-04, 53-00-00 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200 TO 237, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00, 51-10-04 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, LBL 8 TO RBL 8, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT, STA 200, RBL 9 TO RBL 46, CORROSION. ACCOMPLISHED FLOOR SUPPORT REPLACEMENT PER B717 SRM 53-00-00 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SEAT TRACK, STA 200 TO 237, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER B717 SRM 51-10-04 AND 53-20-52.

Part: SIGN — MALFUNCTIONED (CABIN)

AFT BULKHEAD EXIT SIGN COMES ON AND OFF IN FLT. INSP SIGN AND BULB SECURITY AND PERFORMED OPS CHECK IAW AMM 33-51. SIGN OPS NORMAL AT THIS TIME. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS FOR THE ENG NACELLES WILL NOT TURN OFF. REMOVED AND REPLACED BATTERY SUPPLY POWER FOR ENG NACELLES REF MM 33-51. OPS CHECKED GOOD.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

OVERWING EMERGENCY LIGHTS STAY ON. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS EVACUATION BATTERY POWER SUPPLY REF AMM 33-51, OPS CHECK GOOD.

Part: SIGN — MALFUNCTIONED (CABIN)

F/A REPORTS EMERGENCY EXIT SIGN OVER AFT JUMPSEAT FLASHES ON AND OFF. PERFORMED OPERATIONAL CHECK PER B717 AMM 33-51-00. NO FAULTS NOTED. OK FOR SERVICE AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN)

AFT ACCESSORY COMPARTMENT EGRESS PATHWAY EMERG LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATTERY SUPPLY ASSY LOCATED ABOVE / AFT F/A JUMPSEAT IAW B717 AMM CHAPTER 33-51-03.

Part: BATTERY — DISCHARGED (CABIN)

FOUND OVERWING EMER EXIT LIGHT ON BOTH SIDES, AFTER SWITCH TURNED OFF POSITION (VERIFIED BATTERY PACK/PWR SUPPLY IN AFT CARGO / PANEL, OPEN CONNECTOR DISCONNECTED). REMOVED AND REPLACED EMER EXIT BATTERY SUPPLY OPS CHECK GOOD, NO FAULTS NOTED REF M/M 33-51-00, 33-51-06.

Part: INVERTER — MALFUNCTIONED (AC SYSTEM)

BUS A/C EMER OFF ALERT DISPLAYED WITH EMER PWR SW SELECTED TO ARM OR ON. REMOVED AND REPLACED STATIC INVERTER, REF B717 AMM 24-24. OP'S CHECK GOOD NO ALERTS PRESENT.

Part: LIGHT — MALFUNCTIONED (CABIN)

AFT EMERGENCY LIGHT ON WITH SWITCH IN ARM POSITION. C/ B717 FIM 33-50 TASK 801, FAULT CLEARED.

Part: COVER — MISSING (CABIN)

SEAT 2-D EMERGENCY LIGHT COVER MISSING. INSTALLED EMERGENCY LIGHT COVER REF MM 33-50.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT AFT COMPARTMENT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY AND BATTERY ASSEMBLY AT AFT COMPARTMENT.

Part: SKIN — DAMAGED (FUSELAGE)

AT APPROXIMATELY 4000 FEET, AIRCRAFT STRUCK A FLOCK OF BIRDS. RETURNED BACK TO BWI AND LANDED AT APPROXIMATELY 108,700 LBS. REMOVED DAMAGED SKIN, REMOVED DAMAGED FRAMES. FABRICATED REPAIR SKIN & DOUBLERS IAW B717 SRM DRW SR95530006 & SRM 51.41. INSTALLED 2 EACH FRAMES, REPAIR DOUBLER & SKIN SECTION IAW B717 SRM 51-41. REF REPAIR SRM 53-10-01, REPAIR 8.

Part: DOOR FRAME — CORRODED (CARGO BAY)

AFT CARGO DOOR JAMB PAN, STA 954 TO 994, CORROSION. ACCOMPLISHED JAMB PAN SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7 FIG 201. SEE NR 3422 AND 3532.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2895 AFT RIGHT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 5. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, RIGHT SIDE IAW AIRTRAN TASK CARD 17-5310-2990.

Part: FRAME — DAMAGED (FUSELAGE)

EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 2 CONDITION 4. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2979.

Part: FASTENER — SHEARED (ACCESSORY BAY)

AFT ACCESSORY COMPARTMENT FASTENER, STA 1152, LBL 10, SHEARED. ACCOMPLISHED FASTENER REPLACEMENT PER EA-53-02140IR. SEE NR 3483.

Part: ANGLE — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT ANGLE, STA 1022, LONG L29L TO L30, CORROSION. ACCOMPLISHED ANGLE FRAME REPAIR PER B717 SRM 53-20-07. SEE NR 3509 AND 3538.

Part: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT CIRCUMFERENTIAL, STA 908, LONG L29L TO L29R, CORROSION. ACCOMPLISHED CIRCUMFERENTIAL FRAME REPAIR PER B717 SRM 53-20-07. SEE NR 3460 AND 3535.

Part: BALL — DISLODGED (TAILCONE)

TAIL CONE UNLOCK ALERT IN FLIGHT. FOUND INSIDE BALL ON CABLE TO TAIL CONE SWITCH DISLODGED. REINSTALLED CABLE, LIGHT EXTINGUISHED IN COCKPIT. NO OTHER DISCREPANCIES NOTED PER MM 52-73-01 & 53-52-01.

Part: UNKNOWN — ODOR (AFT CABIN)

ODOR OF SMOKE FROM AFT OF AC BY F/A JUMPSEAT. INSPECTED AFT F/A HANDSET AND CRADLE FOR DEFECTS AS WELL AS THE TAIL CONE AREA AS WELL AS BOTH LAVS FOR OBVIOUS DEFECTS NONE NOTED, RAN A/C AT 1.3 EPR IN NORMAL CONFIG FOR 10-15 MIN. NO DEFECTS CND ON GROUND.

Part: SELECTOR PANEL — INOPERATIVE (FUEL SYSTEM)

AFTER TAKEOFF, NOTICED FUEL MIGRATION IMBALANCE OCCURING. RIGHT TANK WAS +600 LBS. DECLARED EMERGENCY. UPON LANDING FUEL TOTALIZER (X) OUT THEN CAME BACK LATER. REMOVED AND REPLACED LSDU IAW AMM 28-41-20, OPS CHECK GOOD. PN/OFF/ON-366-200-001, SN/OFF-1137, SN/ON-1063.

Part: LINE — BROKEN (LEFT TANK)

AT ABOUT 2100 FT THE ENGINE -LT FUEL PRESS- LIGHT ILLUMINATED. OBSERVED LT TANK FUEL DECREASING AND RT TANK FUEL INCREASING. DECLARED EMERGENCY AND LANDED AT RDU. REPLACED FUEL LINE IN LEFT MAIN TANK M/M 28-22-02. FWD BOOST PUMP VOLUTE PLUMBING. OPS CHECKS GOOD.

Part: SKIN — DENTED (BS 926-948)

ON GATE AFTER POST FLIGHT, RAMP REPORTS A DENT APPROX 18 INCHES IN FRONT OF REAR CARGO DOOR AT BOTTOM OF DOOR LEVEL. CLASS 3 TEMP REPAIR INSTALLED AT LONGERON RIGHT 27 FUSELAGE STATION 926 TO 948. INSPECT EVERY 3000 HRS AND REPLACE AT 8000 HRS REF 717 SRM 53-00-01. INSTALLED DOUBLER REPAIR AT LONGERON 27 RIGHT FUSELAGE 926 TO 948 IAW SRM 51-30-01 REPAIR 1. MATERIAL USED 2075 T6.075 SIZE 19 X 12.5 INCH.